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Presented by:
CHAKANKAR AMOL CHANDRAKANT
BE (MECH)
ROLL NO-120
 Introduction : What is composite?
 Why composite in Aerospace industry?
 Applications of composite in aerospace
 Future involvement of composite
 Conclusion
o Composite is material consisting of two or more
materials, which have different physical and chemical
properties, combined together in a proper content and
fashion to produce a new material properties that are
different from the properties of those individual
materials.
 The main aim of the aerospace/aircraft industries is to
reduce weight keeping the same or more strength
than the regular metals have.
 This criteria leads to use composite.
 Light weight
 High heat resistance
 High strength to weight ratio
 Low density
 Corrosion resistance
 High stiffness
 Fatigue resistance
 Fiber glass
 CFRP
 QFRP
 GFRP
 GLARE
Fuselage (Bulkhead)
Wing flaps
Rudder
Elevators
Radome
Spoilers
Floor beams and panels
Helicopter main and tail rotor blades
Space vehicles: Satellites, Missiles, Rockets etc.
Commercial :
o Boeing 777
o Boeing 787 “Dreamliner”
o Airbus A380
Military:
o B-2 Bomber
o LCA Tejas (HAL)
 Components that uses composite
structure are:
◦ Horizontal Stabilizer
◦ Vertical Fin
◦ Radom
◦ Wing fairings
◦ Passenger floor beams
◦ Wing Box
◦ Engine Cowlings
◦ Engine fairings
 Reduction in weight is over
5800 pounds.
 Components that uses composite structure are:
◦ Almost full fuselage
◦ Upper and lower wing skin
◦ Radom
◦ Wing flaps, elevators, ailerons
◦ Vertical Fin and Horizontal Stabilizer
 Use of composite is 80% by volume and 50% by weight.
 Components that uses composite
structure are:
◦ Horizontal Stabilizer
◦ Vertical Fin
◦ Radom
◦ Wing Fairings
◦ Wing Box
◦ Belly Fairings
◦ Engine Cowlings
◦ Engine fairings
 Wing box, made of CFRP, has reduced
weight up to one and a half tones.
 B-2 Bomber is mostly made of
carbon/epoxy materials.
 The reduction in weight was
about 40000 to 50000 pounds.
 Design material was specially
designed to absorb radar
waves.
 LCA stands for Light Combat Aircraft which is basically use of composite
materials in its structure.
 Components which are made of composite material are:
◦ Nose
◦ Wing upper surface and leading edge
◦ Exit Nozzle
 Weight is reduced by 21%
 Used to manufacture Rocket and Missiles motor cases.
Materials for this are carbon, aramid and glass.
 Composites like carbon-carbon are used to manufacture
re-entry nose tips and heat shields.
 Use of composite is more challenging to design.
 NDT test for composite material is much more difficult as
compared to metals.
 Delamination of layers.
 High cost
 Damage tolerance.
 Need specialized repair techniques.
Honeycomb Structure
 Honeycomb Structure
 Hybrid composite materials
 Advanced Designs through
Simulation
 Investigations into damage
tolerance of bonded repairs
by test and simulation.
 Since the invention of composite materials, aerospace industry
has shown significant use of it in building different parts first
to almost most of the structural parts and use of it is rapidly
growing.
 The main aspect we need to keep in mind that strength and
stiffness are major considerations for aircrafts whereas
stiffness and low coefficient of thermal expansion are major
considerations for space applications.
Thank You

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Application of composite materials in aerospace industry

  • 1. Presented by: CHAKANKAR AMOL CHANDRAKANT BE (MECH) ROLL NO-120
  • 2.  Introduction : What is composite?  Why composite in Aerospace industry?  Applications of composite in aerospace  Future involvement of composite  Conclusion
  • 3. o Composite is material consisting of two or more materials, which have different physical and chemical properties, combined together in a proper content and fashion to produce a new material properties that are different from the properties of those individual materials.
  • 4.  The main aim of the aerospace/aircraft industries is to reduce weight keeping the same or more strength than the regular metals have.  This criteria leads to use composite.
  • 5.  Light weight  High heat resistance  High strength to weight ratio  Low density  Corrosion resistance  High stiffness  Fatigue resistance
  • 6.
  • 7.  Fiber glass  CFRP  QFRP  GFRP  GLARE
  • 8. Fuselage (Bulkhead) Wing flaps Rudder Elevators Radome Spoilers Floor beams and panels Helicopter main and tail rotor blades Space vehicles: Satellites, Missiles, Rockets etc.
  • 9. Commercial : o Boeing 777 o Boeing 787 “Dreamliner” o Airbus A380 Military: o B-2 Bomber o LCA Tejas (HAL)
  • 10.  Components that uses composite structure are: ◦ Horizontal Stabilizer ◦ Vertical Fin ◦ Radom ◦ Wing fairings ◦ Passenger floor beams ◦ Wing Box ◦ Engine Cowlings ◦ Engine fairings  Reduction in weight is over 5800 pounds.
  • 11.  Components that uses composite structure are: ◦ Almost full fuselage ◦ Upper and lower wing skin ◦ Radom ◦ Wing flaps, elevators, ailerons ◦ Vertical Fin and Horizontal Stabilizer  Use of composite is 80% by volume and 50% by weight.
  • 12.  Components that uses composite structure are: ◦ Horizontal Stabilizer ◦ Vertical Fin ◦ Radom ◦ Wing Fairings ◦ Wing Box ◦ Belly Fairings ◦ Engine Cowlings ◦ Engine fairings  Wing box, made of CFRP, has reduced weight up to one and a half tones.
  • 13.  B-2 Bomber is mostly made of carbon/epoxy materials.  The reduction in weight was about 40000 to 50000 pounds.  Design material was specially designed to absorb radar waves.
  • 14.  LCA stands for Light Combat Aircraft which is basically use of composite materials in its structure.  Components which are made of composite material are: ◦ Nose ◦ Wing upper surface and leading edge ◦ Exit Nozzle  Weight is reduced by 21%
  • 15.  Used to manufacture Rocket and Missiles motor cases. Materials for this are carbon, aramid and glass.  Composites like carbon-carbon are used to manufacture re-entry nose tips and heat shields.
  • 16.  Use of composite is more challenging to design.  NDT test for composite material is much more difficult as compared to metals.  Delamination of layers.  High cost  Damage tolerance.  Need specialized repair techniques.
  • 17. Honeycomb Structure  Honeycomb Structure  Hybrid composite materials  Advanced Designs through Simulation  Investigations into damage tolerance of bonded repairs by test and simulation.
  • 18.  Since the invention of composite materials, aerospace industry has shown significant use of it in building different parts first to almost most of the structural parts and use of it is rapidly growing.  The main aspect we need to keep in mind that strength and stiffness are major considerations for aircrafts whereas stiffness and low coefficient of thermal expansion are major considerations for space applications.